View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 26960U 01049D 23151.83479505 .00007538 00000-0 39386-3 0 9995
2 26960 97.7832 182.5549 0045599 327.0396 32.7994 15.15290126181979
Epoch (UTC): | 31 May 2023 20:02:06 |
Eccentricity: | 0.0045599 |
inclination: | 97.7832° |
perigee height: | 488 km |
apogee height: | 551 km |
right ascension of ascending node: | 182.5549° |
argument of perigee: | 327.0396° |
revolutions per day: | 15.15290126 |
mean anomaly at epoch: | 32.7994° |
orbit number at epoch: | 18197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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